In the article on the LA-46 in the November issue of Aero Modeller, Maris Dislers talks about the transfer ports. He says—
'I doubt that Doctor Schnuerle would have acknowledged the arrangement as meeting his idea for loop scavenging. Rather, combustion residues on the piston crown suggest the system works more like the reverse-flow pattern seen in Cox engines.'
Can anybody explain this reverse flow in Cox engines for me, please?